WO2006108579B1 - Single slotted flap with sliding deflector flap and lowerable spoiler - Google Patents
Single slotted flap with sliding deflector flap and lowerable spoilerInfo
- Publication number
- WO2006108579B1 WO2006108579B1 PCT/EP2006/003212 EP2006003212W WO2006108579B1 WO 2006108579 B1 WO2006108579 B1 WO 2006108579B1 EP 2006003212 W EP2006003212 W EP 2006003212W WO 2006108579 B1 WO2006108579 B1 WO 2006108579B1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- slot
- high lift
- wing element
- slot covering
- lift device
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C2009/143—Adjustable control surfaces or members, e.g. rudders forming slots comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge flaps
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
- Toys (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Mechanical Control Devices (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
Claims
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200680011499XA CN101155726B (en) | 2005-04-11 | 2006-04-07 | Device and method for adjusting lift characteristic of aircraft |
US11/911,124 US8066228B2 (en) | 2005-04-11 | 2006-04-07 | Single slotted flap with sliding deflector flap and lowerable spoiler |
DE602006019702T DE602006019702D1 (en) | 2005-04-11 | 2006-04-07 | SINGLE-FOLDING FLAP WITH SLIDING REAR FLAP AND SLEEPABLE SPOILER |
BRPI0607925-3A BRPI0607925A2 (en) | 2005-04-11 | 2006-04-07 | single slotted flap with sliding deflector flap and lowering spoiler |
JP2008504700A JP5185105B2 (en) | 2005-04-11 | 2006-04-07 | Single slotted flap with sliding deflector flap and lowering spoiler |
CA2598419A CA2598419C (en) | 2005-04-11 | 2006-04-07 | Single slotted flap with sliding deflector flap and lowerable spoiler |
EP06724150A EP1868887B1 (en) | 2005-04-11 | 2006-04-07 | Single slotted flap with sliding deflector flap and lowerable spoiler |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US67020105P | 2005-04-11 | 2005-04-11 | |
US60/670,201 | 2005-04-11 | ||
DE102005016578A DE102005016578A1 (en) | 2005-04-11 | 2005-04-11 | Airplane`s lift characteristics adjusting device, has spoiler devices movably fastened at wing unit and/or at high lift device, where spoiler devices are designed such that size of gap between wing unit and high lift device is adjusted |
DE102005016578.8 | 2005-04-11 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2006108579A1 WO2006108579A1 (en) | 2006-10-19 |
WO2006108579B1 true WO2006108579B1 (en) | 2007-01-11 |
Family
ID=37055256
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2006/003212 WO2006108579A1 (en) | 2005-04-11 | 2006-04-07 | Single slotted flap with sliding deflector flap and lowerable spoiler |
Country Status (9)
Country | Link |
---|---|
US (1) | US8066228B2 (en) |
EP (1) | EP1868887B1 (en) |
JP (1) | JP5185105B2 (en) |
CN (1) | CN101155726B (en) |
BR (1) | BRPI0607925A2 (en) |
CA (1) | CA2598419C (en) |
DE (2) | DE102005016578A1 (en) |
RU (1) | RU2399553C2 (en) |
WO (1) | WO2006108579A1 (en) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006053259A1 (en) * | 2006-11-11 | 2008-05-21 | Airbus Deutschland Gmbh | High-lift system on the wing of an aircraft and method for its operation |
US7874524B2 (en) * | 2007-11-16 | 2011-01-25 | The Boeing Company | Methods and apparatus for a multi-segment flap fence |
FR2929724B1 (en) * | 2008-04-02 | 2010-04-30 | Airbus France | METHOD FOR DETERMINING THE FLOOD OUTPUT SPEED OF AN AIRCRAFT. |
GB0810724D0 (en) * | 2008-06-12 | 2008-07-16 | Airbus Uk Ltd | Slat assembly |
DE102008033005A1 (en) * | 2008-07-14 | 2010-03-18 | Airbus Deutschland Gmbh | Aerodynamic flap and wings |
US8424810B1 (en) | 2010-03-31 | 2013-04-23 | The Boeing Company | Low noise wing slat system with rigid cove-filled slat |
US8276852B2 (en) * | 2010-03-31 | 2012-10-02 | The Boeing Company | Low noise wing slat system with deployable wing leading edge elements |
US8864083B1 (en) | 2010-03-31 | 2014-10-21 | The Boeing Company | Low noise wing slat system with a fixed wing leading edge and deployable bridging panels |
GB201117340D0 (en) | 2011-10-07 | 2011-11-23 | Airbus Uk Ltd | Flat support |
GB2512318A (en) * | 2013-03-26 | 2014-10-01 | Eads Uk Ltd | Lift-reducing apparatus for aircraft wings |
US10000274B2 (en) * | 2015-08-20 | 2018-06-19 | The Boeing Company | Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft |
US11046425B2 (en) * | 2016-05-20 | 2021-06-29 | Bombardier Inc. | Apparatus and methods for actuating a double-slotted flap using a slave screw |
CN108100223A (en) * | 2017-11-29 | 2018-06-01 | 中国航空工业集团公司西安飞机设计研究所 | A kind of whirlpool paddle aircraft |
GB2579221A (en) * | 2018-11-26 | 2020-06-17 | Airbus Operations Ltd | Aircraft control mechanism |
EP3941828A4 (en) | 2019-03-21 | 2022-11-16 | AMSL Innovations Pty Ltd | Vertical take-off and landing (vtol) aircraft |
CN110866351B (en) * | 2019-09-27 | 2021-07-27 | 南京航空航天大学 | Resistance-increasing micro-texture design of wing spoiler and manufacturing method based on CFRP material |
CN110861767A (en) * | 2019-12-13 | 2020-03-06 | 贵州贵航飞机设计研究所 | Method for combined driving of wing high-lift device |
CN113104196B (en) * | 2021-05-28 | 2022-05-24 | 中国商用飞机有限责任公司 | High-lift device and high-lift method for aircraft |
CN114750930B (en) * | 2022-05-07 | 2023-05-16 | 中国航空工业集团公司沈阳飞机设计研究所 | Airfoil slotted spoiler type course control surface |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2272058A (en) * | 1938-10-18 | 1942-02-03 | Libbey Owens Ford Glass Co | Table top, counter top, or the like |
US2261363A (en) | 1939-04-29 | 1941-11-04 | United Aireraft Corp | Spoiler |
US2700516A (en) | 1950-01-31 | 1955-01-25 | Phiroze P Nazir | Aircraft lift control device |
US2772058A (en) | 1951-05-10 | 1956-11-27 | Charles H Grant | Aircraft wing with means to increase lift through control of air flow |
US2924399A (en) * | 1956-04-23 | 1960-02-09 | North American Aviation Inc | Aircraft flap structure |
US2920844A (en) * | 1957-04-12 | 1960-01-12 | North American Aviation Inc | Aircraft boundary-layer control system |
US2987277A (en) * | 1958-10-14 | 1961-06-06 | North American Aviation Inc | Aircraft control system |
US3131873A (en) * | 1963-07-29 | 1964-05-05 | Ryan Aeronautical Co | Ejector flap system for aircraft wing with ducted fan |
DE1813407C3 (en) | 1968-12-07 | 1974-07-25 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Airfoil for aircraft with at least one main flap located on the wing trailing edge |
DE1943037C3 (en) | 1969-08-23 | 1978-08-24 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Wing for aircraft, consisting of main wing and slat |
DE1943680C2 (en) * | 1969-08-28 | 1982-06-24 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | Control flap arrangement |
DE2216710A1 (en) * | 1972-04-07 | 1973-10-18 | Dornier Gmbh | COVER SHIELD FOR FLOW-EFFICIENT COVERING OF SURFACE OPENINGS IN COMPONENTS, IN PARTICULAR OF OPENINGS ON PARTS OF AIRCRAFT EQUIPMENT |
US3757121A (en) * | 1972-04-17 | 1973-09-04 | Ulmic Sa | Movement of a movable component of an airplane |
US3897029A (en) | 1973-07-09 | 1975-07-29 | Alberto Alvarez Calderon | Variable camber multi-slotted flaps |
US3921942A (en) * | 1974-07-01 | 1975-11-25 | Gen Dynamics Corp | Rudder boundary layer control device |
US4784355A (en) | 1986-11-10 | 1988-11-15 | The United States Of America As Represented By The Secretary Of The Air Force | Flap system for short takeoff and landing aircraft |
US4905934A (en) * | 1988-07-05 | 1990-03-06 | Grumman Aerospace Corporation | Universal-type gust alleviation system for aircraft |
JPH05238488A (en) | 1992-02-28 | 1993-09-17 | Mitsubishi Heavy Ind Ltd | Directional control device for aircraft |
DE4334680C2 (en) | 1993-10-12 | 1996-07-11 | Daimler Benz Aerospace Airbus | Device for adjusting gap control flaps |
FR2728535A1 (en) * | 1994-12-26 | 1996-06-28 | Aerospatiale | VARIABLE SLOTTED AEROBRAKE FOR AIRCRAFT WING |
WO1996036532A1 (en) | 1995-05-19 | 1996-11-21 | Mcdonnell Douglas Corporation | Airfoil lift management device |
US5788190A (en) | 1996-10-22 | 1998-08-04 | The Boeing Company | Slotted cruise trailing edge flap |
RU2187445C1 (en) | 2000-12-15 | 2002-08-20 | Открытое акционерное общество "Туполев" | Device for connection of flaps |
US6601801B1 (en) | 2002-04-24 | 2003-08-05 | The Boeing Company | Gapped trailing-edge control surface for an airfoil |
-
2005
- 2005-04-11 DE DE102005016578A patent/DE102005016578A1/en not_active Withdrawn
-
2006
- 2006-04-07 RU RU2007141590/11A patent/RU2399553C2/en not_active IP Right Cessation
- 2006-04-07 CN CN200680011499XA patent/CN101155726B/en not_active Expired - Fee Related
- 2006-04-07 CA CA2598419A patent/CA2598419C/en not_active Expired - Fee Related
- 2006-04-07 BR BRPI0607925-3A patent/BRPI0607925A2/en not_active IP Right Cessation
- 2006-04-07 US US11/911,124 patent/US8066228B2/en not_active Expired - Fee Related
- 2006-04-07 WO PCT/EP2006/003212 patent/WO2006108579A1/en active Application Filing
- 2006-04-07 EP EP06724150A patent/EP1868887B1/en not_active Expired - Fee Related
- 2006-04-07 JP JP2008504700A patent/JP5185105B2/en not_active Expired - Fee Related
- 2006-04-07 DE DE602006019702T patent/DE602006019702D1/en active Active
Also Published As
Publication number | Publication date |
---|---|
DE602006019702D1 (en) | 2011-03-03 |
BRPI0607925A2 (en) | 2009-10-20 |
CA2598419C (en) | 2013-07-23 |
US8066228B2 (en) | 2011-11-29 |
RU2007141590A (en) | 2009-05-20 |
WO2006108579A1 (en) | 2006-10-19 |
CN101155726A (en) | 2008-04-02 |
CN101155726B (en) | 2013-03-13 |
CA2598419A1 (en) | 2006-10-19 |
JP5185105B2 (en) | 2013-04-17 |
EP1868887A1 (en) | 2007-12-26 |
JP2008535721A (en) | 2008-09-04 |
US20080179464A1 (en) | 2008-07-31 |
EP1868887B1 (en) | 2011-01-19 |
DE102005016578A1 (en) | 2006-10-19 |
RU2399553C2 (en) | 2010-09-20 |
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